Front electric rotor helicopter

ABSTRACT

My invention is a helicopter having a front electric anti-torque rotor for the purpose of having a mechanically driven pusher propeller at the rear for increase forward speed. Speed has been a limiting factor in vertical flight. Various designs have been conceived by people around the world to make the helicopter go faster. My design is a high speed single rotor helicopter design that uses a gas-electric hybrid front electric anti-torque rotor system to allow for a mechanically driven pusher propeller at the rear. As the helicopter go forward, the front electric anti-torque gives control and the mechanically driven pusher propeller at the rear gives increase forward speed. The intent of the design is to make a high speed single rotor helicopter design.

CROSS-REFERENCE TO RELATED APPLICATIONS

This applications claims priority benefit of provisional patentapplication No. 61/493,848, filed 6 Jun. 2010, entitled

“HELICOPTER EMPLOYING AN ANTI-TORQUE ROTOR HAVING A POWER SOURCEINDEPENDENT OF THE POWER SOURCE FOR THE PRIMARY LIFT ROTOR” FIELD OF THEINVENTION

The invention relates to aeronautics in the area of vertical flight.Igor Sikorsky invented the tail rotor helicopter. The tail rotorprovided control for the single rotor helicopter during vertical flight.This invention uses an electric front rotor helicopter design to allowfor a mechanical pusher propeller at the rear to increase the forwardspeed of the helicopter. The pusher propeller at the rear of the singlerotor helicopter is optional. Turn the pusher propeller on for extraspeed or turn it off so virtually all the engine power will go into thelift/efficiency of the helicopter (put this on website and sell/marketit to companies). A switch for speed (propeller turned on) and a switchfor pure lifting power (propeller turned off). This front electric rotorhelicopter design with a mechanical pusher propeller at the rear serveas the basis for a high speed single rotor helicopter design.

BACKGROUND OF THE INVENTION

The Background for this invention is aeronautics concerning anti-torquerotor of the single rotor helicopter. The anti-torque rotor of ahelicopter is used to help control the helicopter during flight.Conventional control for a single rotor helicopter involves the use ofan rear anti-torque rotor to give stability and control. That rearanti-torque rotor is mechanically driven from the engine. As verticalflight technology progress their has been a need to make helicopter flyfaster in the forward direction. Many designs have been put forth fromusing wings and jet engines to make the helicopter go faster to usingco-axial lift rotor with a pusher propeller at the rear to increasespeed. My invention uses a single rotor helicopter that has a frontelectric anti-torque rotor on the nose of the helicopter so amechanically driven pusher propeller can be at the rear to increase theforward speed of the helicopter.

DETAILED DESCRIPTION OF THE INVENTION

The following detailed description is of the best currently contemplatedmodes of carrying out exemplary embodiments of the invention. Thedescription is not to be taken in a limiting sense, but is made merelyfor the purpose of illustrating the general principles of the invention,since the scope of the invention is best defined by the appended claim.

The conventional configuration of a helicopter includes a primary liftrotor to provide lift for the helicopter, and a tail rotor to counteractthe torque generated by the rotation of the primary lift rotor. Theprimary lift rotor is mounted on a shaft above the fuselage, or body, ofthe helicopter. As the primary lift rotor rotates, airflow is createdover the blades of the primary lift rotor, resulting in lift. Typically,tail rotor is employed to produce thrust acting in a directiontransverse to the long axis of the fuselage to prevent the fuselage fromrotating. By increasing or decreasing the thrust produced by the tailrotor, the pilot can steer the helicopter to the left or right.

In the design of conventional helicopters, the tail rotor is powered bythe same primary engine that powers the primary lift rotor, therebypreventing the full power capacity of the primary engine from beingdedicated to lifting the helicopter. The present invention solves thisproblem by incorporating an anti-torque rotor which has an auxiliarypower source that is independent of the primary engine.

Referring now to the drawings, the Figures shows the helicopterconfiguration according to an exemplary embodiment of the invention,comprised of the following elements:

1. a fuselage;

2. a primary lift rotor;

3. a primary engine;

4. an anti-torque rotor;

5. an auxiliary engine;

6. an optional pusher propeller; and

7. An optional pusher engine.

8. A cockpit

9. Retractable landing gear

As in a conventional helicopter configuration, the primary lift rotormay be mounted above the fuselage and may be powered by the primaryengine. Unlike conventional helicopter configuration, the presentinvention may incorporate an anti-torque rotor that may be powered by anauxiliary engine that may be independent of the primary engine. Theauxiliary engine may be a fuel burning engine, an electric motor, or anyuseful means of providing power to the anti-torque rotor.

In the exemplary embodiment shown in Figure, the anti-torque rotor maybe mounted at the front of the fuselage. As an option, a pusherpropeller may be mounted at the aft end of the fuselage to provideadditional forward thrust to the helicopter. The pusher propeller may bepowered by its own dedicated pusher engine or, alternatively, by theauxiliary engine.

In an alternative exemplary embodiment, the anti-torque rotor may bemounted at the rear of the fuselage.

It should be understood, of course, that the foregoing relates toexemplary embodiments of the invention and that modifications may bemade without departing from the spirit and scope of the invention as setforth in the following claim.

DRAWING DESCRIPTION

FIG. 1: is a side view of the invention.

FIG. 2: is perspective view of the invention.

FIG. 3: is a top view of the invention.

DESCRIPTION LIST

-   1: Front Anti-torque rotor blades-   2: front hub around anti-torque rotor-   3: Mesh air grill on the left & right side of front rotor-   4: electric motor-   5. Electrical wire from electrical generator to front electric rotor-   6. Electrical generator (auxiliary engine)-   7. Gear-   8. Rear landing wheel container-   9. Drive shaft from primary life engine to rear pusher propeller-   10. Rear pusher propeller-   11. Front cockpit-   12. Primary lift blade-   13. Primary lift engine.

BRIEF SUMMARY OF THE INVENTION

This invention is a front electric rotor helicopter design to allow fora mechanical pusher propeller at the rear for increase forward speed.The gas engine of the single rotor helicopter is also used to spin anelectric generator to power the front electric anti-torque rotor. Byhaving this gas-electric hybrid front electric rotor system allows for amechanically drive pusher propeller at the rear. This helicopter designis intended to make the single rotor helicopter much faster in forwardspeed than a conventional tail rotor helicopter.

1. A helicopter comprising: a fuselage; a primary lift rotor mountedabove said fuselage to provide lift for said helicopter; and
 2. Thehelicopter of claim 1, a primary lift rotor having a power sourceindependent of the power source for said conventional gas powered engine3. The helicopter of claim 1, an anti-torque rotor mounted alternativelyat the front or the rear of said fuselage to counteract the torqueinduced by the primary lift rotor, said anti-torque rotor having a powersource independent or dependent of the power source for said primarylift rotor.